This N-number isn't registered right now. Below is its last known registration, canceled Jan 29, 2013.
Safety record in brief:1 NTSB incident (minor damage, Feb 2004)No ADs since 1998 matched3 service difficulty reports
We never show street addresses, even though they appear in the public FAA file. Individual owners are shown by city and state only.
Total time and engine hours aren't public. They appear here once the owner adds logbooks.
Individual owners are shown by city and state only.
the tail rotor pitch change lever failed in fatigue due to improper installation by company maintenance personnel.
From NTSB records; matched by N-number.Read NTSB report (search CAROL for LAX04IA133)
These match the airframe or engine model. Whether each one applies, and whether it's been complied with, depends on serial numbers, equipment and logbook entries. Applicability must be confirmed by a mechanic against the aircraft's records.
No ADs published since 1998 matched this airframe or engine model.
AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.
Reports of failures and defects that operators and repair stations sent to the FAA since 1995. A report describes one finding; it is not an accident.
EMERGENCY ACTIONS EXC. ENGINE SHUTDOWN AT CRUISE AT APPROX. 110 KTS PILOT FELT THE AIRCRAFT YAW. PUSHING IN T/R PEDALS HAD NO EFFECT. PILOT CONTINUED STRAIGHT AND LEVEL FLIGHT TO MAIN BASE AND NOTIFIED COMPANY OF SITUATION. AFTER 5 ABORTED ATTEMPTS PILOT EXECUTED A RUN ON LANDING AND BROUGHT THE…
From FAA Service Difficulty Reports; matched by N-number and serial number.TAIL ROTOR TRIM TAB DEBONDED APPROXIMATELY 90 MM ON BOTH SIDES, STARTING ON THE INBOARD END. TAIL ROTOR INSTALLED. FOUND ON PREFLIGHT, POSSIBLE IMPROPER BONDING DURING MANUFACTURE. PART RETURNED TO MFG FOR EVALUATION.
From FAA Service Difficulty Reports; matched by N-number and serial number.AIRCRAFT IN FLIGHT EXPERIENCED HYDRAULIC LIGHT AND THEN HYDRAULIC FAILURE. AIRCRAFT SAFELY RETURNED TO AIRPORT AND LANDED. FAILURE OF HYDRAULIC BELT AT THE JOINING SEAM WAS THE CAUSE OF FAILURE.
From FAA Service Difficulty Reports; matched by N-number and serial number.